ARKTIKA-M 2, 58584
Orbit data source: Space-Track
ARKTIKA-M 2, 58584 is a payload satellite owned by Roskosmos (CIS) in HEO that was launched on Sat, 16 Dec 2023 UTC via a SOYUZ-2-1B launch vehicle from the Tyuratam Missile And Space Complex (TTMTR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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58584 intel report (Beta)
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Identifier
Orbit
Country
CISRelated business
Manufacturer
Lavochkin
Mission
Operational Civil Weather
Bus & Motor
NAVIGATOR, Unknown motor
Mass
2,200 kg wet, ~2,000 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 5.0 m
Radar Cross Section
14.304 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 5 days ago
TLE from 5 days ago
0 ARKTIKA-M 2
1 58584U 23198A 26168.75920439 .00000145 00000-0 00000-0 0 9995
2 58584 63.2243 154.2920 6902344 267.4286 18.7609 2.00612717 18330Epoch: 2026-06-17T18:13Z
TLE epoch observation values (Epoch: 2026-06-17T18:13:15.259Z)
Latitude
-0.00006°
Longitude
-25.06186°
Altitude
7,988.711 km
Speed
6.363 km/s
True Right ascension
10h 17m 03s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
23:26:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
38,506.33 km
Perigee altitude
1,847.742 km
Semi-major axis
26,555.173 km
Eccentricity
0.69023
Inclination
63.2243°
RAAN
154.292°
Arg. of periapsis
267.4286°
True anomaly
92.62162°
Mean anomaly
18.7609°
Eccentric anomaly
48.27889°
Mean motion
0.50156 °/min
Orbital period
717.77 mins
BSTAR
0
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Other satellites on launch #198 in the year 2023 (2023-12-16 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.ARKTIKA-M 2 Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 189 mins | 2026-06-22 12:24:31.213Z | 326.67° NNW | 2026-06-22 12:24:31.213Z | 326.67° NNW | 23.259° | 2026-06-22 15:33:31.213Z | 302.936° NW |
| 522 mins | 2026-06-22 18:51:31.213Z | 63.84° ENE | 2026-06-22 22:46:31.213Z | 35.26° NE | 27.03° | 2026-06-23 03:33:31.213Z | 58.013° ENE |
| 310 mins | 2026-06-23 07:14:31.213Z | 306.438° NW | 2026-06-23 12:09:31.213Z | 327.047° NNW | 23.278° | 2026-06-23 12:24:31.213Z | 326.49° NNW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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